Index

Navy Terrier LEAP Third-Stage Propulsion

Filename MIME Type Size (Bytes)
ADA288615.pdf  application/pdf 886644




AD Number: ADA288615
Subject Categories: ANTIMISSILE DEFENSE SYSTEMS GUIDED MISSILE TRAJ, ACCURACY AND BALLISTICS SURFACE-LAUNCHED GUIDED MISSILES
Corporate Author: THIOKOL CHEMICAL CORP ELKTON MD
Title: Navy Terrier LEAP Third-Stage Propulsion,
Personal Authors: Olsen, K. E.; Walsh, J. J.; Thomas, E. L.
Report Date: NOV 1994
Pages: 8 PAGES
Monitor Acronym: XD
Monitor Series: BMDO
Supplementary Note: Presented at AIAA Missile Sciences Conference Held at Monterey, California on November 7-9, 1994.
Descriptors: *ANTIMISSILE DEFENSE SYSTEMS, *GUIDED MISSILE TRAJECTORIES, *SURFACE TO AIR MISSILES, TEST AND EVALUATION, GUIDED MISSILES, FLIGHT TESTING, AIR FORCE, ATTITUDE CONTROL SYSTEMS, ORGANIZATIONS, NAVY, CABLES, SOLIDS, PROPELLANTS, PROPULSION SYSTEMS, COMPANY LEVEL ORGANIZATIONS, CALIFORNIA, AIR FORCE FACILITIES, CONNECTORS, MOTORS, THIRD STAGE ENGINES, THRUST VECTOR CONTROL SYSTEMS.
Identifiers: LEAP(LIGHTWEIGHT EXOATMOSPHERIC PROJECTILE), TERRIER MISSILES, 4.
Abstract: Under contracts with the Air Force Phillips Laboratory (Edwards Air Force Base, California) and Hughes Missiles Systems Company, the Elkton Division of Thiokol Corporation has completed the design, development, and qualification of a third stage for use in the Ballistic Missile Defense Organization (BMDO)/ navy Terrier Lightweight Exoatmospheric Projectile (LEAP) flight experiments. The stage consists of a solid- propellant motor with omni-axis thrust vector control (TVC), safe-and-arm (S&A) devices, flight-termination system, pitch/yaw/ roll attitude control system (ACS), cables/connectors, and skirt/interstage structures. The motor with these components is designated as the advanced solid axial stage (ASAS). This paper describes the design, requirements, and results of component- and system- level testing to qualify the stage for the flight tests (FTV-3 and FTVA) scheduled for December 1994 - January 1995.
Limitation Code: APPROVED FOR PUBLIC RELEASE
Source Code: 348950
IAC Document Number: gc-970119
IAC Subject Terms: G--(U)ANTIMISSILE DEFENSE SYSTEMS, GUIDED MISSILE TRAJECTORIES, SURFACE TO AIR MISSILES, TEST AND EVALUATION, GUIDED MISSILES, FLIGHT TESTS, ATTITUDE CONTROL, PROPELLANTS, PROPULSION SYSTEMS, THRUST VECTOR CONTROL, LEAP(LIGHTWEIGHT EXOATMOSPHERIC PROJECTILE), TERRIER MISSILES, CONTROL SYSTEMS.;